FIELD: aircraft engineering.
SUBSTANCE: invention relates to helicopter external load sling systems. Proposed system comprises at least three radial beams (1) fastened to helicopter fuselage bottom (2). Aforesaid beams have eyes (3) to sling ropes (4) of the system. Lower end of the said ropes are furnished with grippers (5) clipped to hoisting members (6) basket (7) accommodating cargo (8).
EFFECT: elimination of cargo rocking at all flight conditions.
3 dwg
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